US3559274A - Process for the sheathing of tubular nuclear fuel elements - Google Patents

Process for the sheathing of tubular nuclear fuel elements Download PDF

Info

Publication number
US3559274A
US3559274A US570024A US3559274DA US3559274A US 3559274 A US3559274 A US 3559274A US 570024 A US570024 A US 570024A US 3559274D A US3559274D A US 3559274DA US 3559274 A US3559274 A US 3559274A
Authority
US
United States
Prior art keywords
sheathing
pipe
fuel
uranium
fuel element
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US570024A
Inventor
Saverio Granata
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SnamProgetti SpA
Original Assignee
SnamProgetti SpA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SnamProgetti SpA filed Critical SnamProgetti SpA
Application granted granted Critical
Publication of US3559274A publication Critical patent/US3559274A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21CNUCLEAR REACTORS
    • G21C21/00Apparatus or processes specially adapted to the manufacture of reactors or parts thereof
    • G21C21/02Manufacture of fuel elements or breeder elements contained in non-active casings
    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21CNUCLEAR REACTORS
    • G21C21/00Apparatus or processes specially adapted to the manufacture of reactors or parts thereof
    • G21C21/02Manufacture of fuel elements or breeder elements contained in non-active casings
    • G21C21/08Manufacture of fuel elements or breeder elements contained in non-active casings by a slip-fit cladding process by crimping the jacket around the fuel
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00Energy generation of nuclear origin
    • Y02E30/30Nuclear fission reactors
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49863Assembling or joining with prestressing of part
    • Y10T29/49865Assembling or joining with prestressing of part by temperature differential [e.g., shrink fit]

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Manufacturing & Machinery (AREA)
  • Plasma & Fusion (AREA)
  • General Engineering & Computer Science (AREA)
  • High Energy & Nuclear Physics (AREA)
  • Monitoring And Testing Of Nuclear Reactors (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Inorganic Compounds Of Heavy Metals (AREA)

Abstract

A TUBULAR NUCLEAR FUEL ELEMENT IS GIVEN AN INTERNAL SHEATING BY THRUSTING A PIPE, SHRUNK BY COOLING, INTO THE ELEMENT AND THEN RAISING THE TEMPERATURE OF THE PIPE TO ROOM TEMPERATURE SO THAT IT EXPANDS AND PASSES TIGHTLY AGAINST THE INNER WALL OF THE FUEL ELEMENT, AND THERE AFTER THE SHEATING IS HEATED INTERNALLY AND THE FUEL ELEMENT IS COOLED EXTERNALLY TO CAUSE INTER-DIFFUSION AT THE INTERFACE BETWEEN THE SHEATHING MATERIAL AND THE FUEL ELEMENT WITHOUT ESTABLISHING PREFERENTIAL CRYSTALLINE ORIENTATIONS IN THE FUEL.

Description

s'.v GRANATA Feb; 2,"1971 PROCESS vFOR THE JHEATHING OF'v TUBULAR NUCLEAR .FUEL ELEMENTS Filed Aug. 5.1966
2 Sheets-Sheet 1 Cnr,
INVENTOR.
F05 2 1971 s. GRANATA 3,559,274
PROCESS FOR THE SHEATHING 0F TUBULAR NUCLEAR FUEL ELEMENTS wed Aug. s. "lese z sheets-sheet s INVENTUR.
United States Patent O 3,559,274 PROCESS FOR THE SHEATHING OF TUBULAR NUCLEAR FUEL ELEMENTS Saverio Granata, Milan, Italy, assignor to Snam Progetti S.p.A., Milan, Italy Filed Aug. 3, 1966, Ser. No. 570,024 Claims priority, apllcatigysltaly, Aug. 6, 1965,
U.S. Cl. 29-447 4 Claims ABSTRACT OF THE DISCLOSURE A tubular nuclear fuel element is given an internal sheathing by thrusting a pipe, shrunk by cooling, into the yelement and then raising the temperature of the pipe to room temperature so that it expands and presses .tightly against the inner wall of the fuel element; and thereafter the sheathing is heated internally and the fuel element is cooled externally to cause inter-diffusion at the interface between the sheathing material and the fuel element without establishing preferential crystalline orientations in the fuel.
profile, it is necessary therefore to use further mechanical working (turning) producing in this way a considerable amount of waste which, being mixed with zirconium, may not be directly utilized again, and has to be sent to chemical purification plants, the same occurring to all the other waste such as: badly done coextrusions, elements lacking in complete adhesion between sheathing The present invention refers to a process of protective sheathing for tubular elements of nuclear fuel used in nuclear reactors.
It is known that one of the main problems concerning the protective sheathing of the nuclear fuels consists in the production of elements wherein a perfect and lasting adhesion between fuel and sheathing material is required.
Particularly, if use is made of tubular nuclear fuel elements, this problem becomes very important especially if the protective sheathing is required to be inside the uranium pipe.
Generally, for the production of this type of nuclear fuel elements use is made of simultaneous coextrusion of the fuel and of the sheathing material.
This prior practice, although allowing the production of nuclear fuel elements which may be particularly long (about 3.5 metres), has the disadvantage of promoting, e.g., in case metallic uranium is used as fuel, a marked preferential crystalline orientation which gives particu larly harmful results when the material is subjected to radiation.
Such a system comprises a considerable number of working stages, such as thermal treatments and mechanical treatments which are characteristic of the coextrusion processes and moreover said treatments have to be carefully controlled in order to prevent deteriorations of the chemical or chemical-physical nature of the fissile material.
For example, in order to prevent the oxidation of said material, use is made during the working stages of metallic sheathings (of copper), said sheathings being later carefully removed by means of chemical processes such as dissolving with acids.
Such a process besides being, as above mentioned, remarkably complicated, presents systematically the following drawbacks:
(1) Establishment of preferential crystalline orientations in the fuel often not eliminable or not completely eliminable, which provoke a considerable anisotropic growth during the radiation. Said preferential orientation is due to the direct mechanical treatments to which the fissile material was subjected during the working.
(2) In the coextrusion process, it is impossible to maintain the lengthwise, ends enclusive, uniformity of the thickness of the uranium pipe.
As the ends are required, as a rule, to have `an exact and fuel and so on.
The process according to the present invention presents comparatively few operations and is easily performed.
In practice, by means of fusion, fuel is shaped, the surfaces are ground mechanically and pickled, the sheathing pipe is introduced into the fuel pipe, an interdiffusion between the surfaces which are in contact is realized and finally the whole is subjected to a thermal treatment in order to obtain the desired structure in the fuel.
The mechanical operations which may give rise to preferential crystalline orientations on the fuel are avoided.
The greater part of recovered waste material may be used directly by refusion.
Therefore the present invention refers to a process of protective sheathing of metallic nuclear fuel pipes which does not promote the preferential crystalline orientation of the structure of nuclear fuel, said process being a rather easy execution and therefore of lower cost.
Said process allows the internal sheathing of metallic uranium pipes or its alloys being based on the different thermal expansions of the uranium and the sheathing material and gives rise to a perfect adhesion between the two materials.
Moreover, the present invention includes a second operation consisting in a suitable heat treatment promoting always an intermetallic diifusion between the two treated materials, in order to warrant the lasting adhesion between them.
The practice of my invention is illustrated in the accompanying drawings in which:
FIGS. 1A, 1B and 1C are vertical sections of a fuel element and a sheathing pipe therefor diagrammatically illustrating their assembly by internal cooling of the sheathing pipe;
FIG. 2 is a vertical section diagrammatically illustrating apparatus for the internal heating of the sheathing pipe and the external cooling of the fuel element; and
FIG. 3 is a photomicrograph of a cross section of a uranium fuel element sheathed with zirconium in accordance with my invention, showing the interdiffusion zone between the uranium fuel element and the zirconium sheathing pipe.
More precisely the process according to the present invention consists substantially in the following stages:
(l) The introduction of a pipe, sheathing the inside surface of the tubular fuel at temperature between +30 C. and 250 C.
(2) IExpansion of said sheathing pipe, at room temperature.
(3) Interdiifusion between sheathing material and fuel material by heating from the inside, starting from the side of said sheathing metal, and by cooling from the outside, starting from the side of the fuel.
The stages (l) and (2) may occur in two ways:
(a) Shrinking the sheathing pipeby cooling, inserting the shrunken sheathing pipe into the fuel element and letting the two elements adhere perfectly by permitting the internal element to expand by raising its temperature to the room temperature; or
(b) Inserting simply the sheathing pipe, at room temperature, into the fuel element and causing the two elements to adhere perfectly, by plastic deformation of the internal one, by means of mechanical or hydraulic systems.
In the first case, the outside diameter of the sheathing material pipe 2 (for example Zircaloy 20) is chosen in such a way as to undergo by cooling a shrinkage until it becomes slightly smaller (for example of 0.01 mm.) than the inside one of the uranium pipe 1 (FIG. 1A).
The sheathing pipe having a diameter, at room temperature, as above defined, provided with a closure 3 at one end, is filled, e.g., with liquid nitrogen 4 (FIG. 1B).
In these conditions the sheathing pipe undergoes a shrinkage as above mentioned and may enter easily into the uranium pipe (FIG. 1C). After having drawn out the cooling liquid the assemblage of said pipes is brought again to room temperature, obtaining in such a way a perfect adherence between the two surfaces, face to face, Of the materials because of the thermal expansion of the inside pipe.
lIn the second case, the diameter of the inside pipe, is suitably chosen according to the above mentioned conditions, taking into account that the temperature at which the pipe is inserted does not fall below -80 C. and preferably is just the room temperature. After the inserting, an expansion of the inside pipe is effected by means of mechanical drawing or other means suitable to this purpose as, for example, hydraulic pressure to obtain the perfect adhesion of the surfaces in contact.
Further possibility is the combination comprising the introduction of the cooled, shrunken sheathing pipe into the fuel element and an additional expansion of the sheathing pipe after it has reached room temperature by drawing.
The cold sheathing process according to the invention presents the great advantage, as to the ones in which the heating of the uranium is effected, of avoiding completely the oxidation of said metal, said oxidation is extremely harmful for the subsequent process of metallic interdiffusion.
The two above mentioned stages are followed by the stage of interdiffusion by heating from the inside and by cooling from the outside.
By means of heating effected from the inside of the two pipes, as shown in FIG. 2, and, i.e., taking advantage, in a suitable way, of the coefficients of thermal expansion of the two materials in function of the radial thermal gradient, produced by means of an outside cooling, the intermetallic diffusion is obtained, said diffusion warrants the lasting adhesion 'between the two materials without presenting harmful drawbacks.
More particularly FIG. 2 shows:
The uranium pipe.
The sheathing material pipe.
A heating element.
A drilled wall allowing the injection of a cold gas.
Finally the fissile material and the sheathing one undergo a conventional thermal treatment in order to give the fissile material the more suitable metallurgic structure necessary for a suitable behaviour of the material in the reactor.
The fuel element so sheathed has shown to be perfectly efficient in the sense that even if subjected to stresses of thermal-mechanical type, it has presented neither disjunction between the two materials so welded nor structural variations during said tests.
The fuel so obtained is produced without preferential crystalline orientations which is an important feature of the element produced according to the present invention and this represents a noticeable advantage of the above mentioned process.
As elements constituting the nuclear fuel there may be used: the adjusted uranium or its alloys like the ones based on uranium-molydenum, uranium-niobium, uranium-silicon and uranium-chromium, and alloys of the type uranium-thorium or uranium-plutonium or uranium containing other elements in the form of alloys in a dispersed phase and finally fuel materials based on uranium oxide or uranium-carbide and metal-ceramics.
As sheathing materials may be utilized the ones generally used in the technique of nuclear rectors like zirconium and its alloys, steel or aluminium or its alloys.
Part of the present invention is also the use of fuel in the form of superposed discs in order to constitute a substantially tubular element.
Such a form of execution is particularly advantageous when the fuel material consists of ceramic materials or metal-ceramics containing uranium.
The following example is reported only as an indicative and not restrictive example of the invention.
EXAMPLE An uranium pipe of the adjusted type having a length of 200 mm. and an inside diameter of 14 mm. and an outside diameter of 22 mm. and a Zircaloy 20 pipe closed at one end having an inside diameter of 12 mm., an outside diameter of 14.02 mm. and 200 mm. long, are subjected to pickling.
The Zircaloy 20 pipe is filled with liquor nitrogen; after 20 minutes the thermal equilibrium is reached and the Zircaloy pipe is introduced into the uranium pipe.
The liquid nitrogen is taken away and in said conditions the temperature of the Zircaloy pipe rises to room temperature; consequently this pipe, by expanding, adheres perfectly to the fuel element.
The element so obtained is subjected to a diffusion treatment under severe radial thermal gradient.
The inside part of the element so obtained is subjected to a heating at 850 C. by means of electric resistance whilst the outside part is kept at 300 C. through a stream of argon.
After a suitable time the heating is discontinued and the whole is brought again to room temperature.
Thereafter the sheathed system was subjected to an examination of the uniformities of the diffusion between the two layers by cutting the sample and by observing it by means of physical-metallurgical systems.
A cross section is shown in FIG. 3 (7 represents the zirconium, 8 the uranium and 9 the diffusion zone).
The X-ray analysis by means of the polar figures has detected the nonexistence of preferential crystalline orientations.
Moreover, some samples drawn either along the axis of the uranium pipe or perpendicularly to said axis have shown a thermal expansion coefficient of 13.10-6 for C., between 0 and 200 C.
The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:
1. Process for the inside sheathing of a tubular fuel element selected from the group consisting of adjusted uranium, alloys of uranium based on molybdenum, niobium, silicon, and chromium, uranium alloys in a dispersed phase, alloys of uranium-thorium and uranium-plutonium, uranium oxides, uranium carbides and metal-ceramic alloys of uranium, comprising:
(a) sheathing the inside surface of a tubular fuel element with a metallic sheathing pipe, at a temperature within the range between +30 and 250 C.
(b) then expanding said sheathing pipe at room temperature;
(c) thereafter causing interdiffusion at the interface of the sheathing metal and the fuel element by heating from the inside, starting from the side of said sheathing metal, and by cooling from the outside, starting from the side of said fuel element.
2. Process according to claim 1 consisting in that the inserting of the sheathing pipe is achieved by shrinkage of the latter by means of cooling at low temperature in the range between -250 C. and 80 C.
3. Process as in claim 2 consisting in shrinking the sheathing element by cooling with a coolant bath at temperatures in the range between 200 C. and 80 C.,
inserting said element in the shrunken state into the tubular fuel element and in expanding subsequently in order to reach the perfect adhesion of the two elements, said expansion being obtained by raising the temperature from that of shrinkage to that of the room.
4. Process according to claim 1 consisting in that the sheathing element is inserted at a temperature between -80 C. and 30 C. in the fuel element, said sheathing element being brought subsequently to a room temperature and nally being expanded by plastic deformation by means of a mechanical treatment at said temperature.
References Cited UNITED STATES PATENTS 1,078,906 1/1913 Eldred 20-473.5 1,193,667 8/1916 Corey 29/474.4 2,713,196 7/1955 Brown 29-497.5 X 2,967,139 1/ 1961 BartOSZak 29'-473.5 3,025,596 3/1962 Ward 29-474.5 X
6 Roseberry 29-474`.4 Reed 29-471.5 Gauthron 29-474.3 Bange 29-498 X Baque 29-474.3
FOREIGN PATENTS Sweden. Germany. yGreat Britain. Germany. Germany.
CHARLIE T. MOON, Primary Examiner 15 R. B. LAZARUS, Assistant Examiner U.S. C1. X.R.
P05 UNITED STATES PATENT OFFICE We CERTIFICATE 0F CORRECTION Patent NQ, Dated February 2, 1.971
Inventod) Saverio Granata It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
Column l, line 75, correct 800C." to read 80C.
Signed and sealed this 12th day of February 1974.
(SEAL) Attest:
EDWARD M.FLET( HER,JR. C. MARSHALL DANN Attestlng Offlcer Commissioner of Patents
US570024A 1965-08-06 1966-08-03 Process for the sheathing of tubular nuclear fuel elements Expired - Lifetime US3559274A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT1776865 1965-08-06

Publications (1)

Publication Number Publication Date
US3559274A true US3559274A (en) 1971-02-02

Family

ID=11150921

Family Applications (1)

Application Number Title Priority Date Filing Date
US570024A Expired - Lifetime US3559274A (en) 1965-08-06 1966-08-03 Process for the sheathing of tubular nuclear fuel elements

Country Status (4)

Country Link
US (1) US3559274A (en)
BE (1) BE685169A (en)
GB (1) GB1156977A (en)
NL (1) NL6611099A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3918623A (en) * 1974-05-07 1975-11-11 Ebara Mfg Method of joining by diffusion welding a hollow part of nonferrous metal onto the inner surface of a hollow part of ferrous metal
US4152816A (en) * 1977-06-06 1979-05-08 General Motors Corporation Method of manufacturing a hybrid turbine rotor
US4186473A (en) * 1978-08-14 1980-02-05 General Motors Corporation Turbine rotor fabrication by thermal methods
US4209896A (en) * 1976-04-02 1980-07-01 Texas Instruments Incorporated Method of assembly of an anti-corrosion anode connector system
DE3007718A1 (en) * 1979-03-05 1980-09-11 Sybron Corp STIRRER WITH A REMOVABLE BLADE UNIT AND METHOD FOR ITS ASSEMBLY
US4231507A (en) * 1979-01-09 1980-11-04 The United States Of America As Represented By The United States Department Of Energy High-temperature, high-pressure bonding of nested tubular metallic components
US4314396A (en) * 1979-03-05 1982-02-09 Sybron Corporation Separable blade agitator assembly and disassembly method
WO1989006583A1 (en) * 1988-01-14 1989-07-27 Electric Power Research Institute, Inc. High pressure bonding process
US4899923A (en) * 1988-01-14 1990-02-13 Electric Power Research Institute, Inc. High pressure bonding process
US5988484A (en) * 1998-03-20 1999-11-23 Osborn; Donald Clad tubular product and method of manufacturing same
US20100126999A1 (en) * 2008-11-21 2010-05-27 Gm Global Technology Operations, Inc. High pressure tank and method thereof
US20120180299A1 (en) * 2009-07-10 2012-07-19 Progressive Ip Ltd. Integrity of the union between components

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111791018B (en) * 2020-08-26 2021-09-17 中铁十八局集团有限公司 Automatic assembling equipment for inner and outer barrels of central sleeve of shield cutter head

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3918623A (en) * 1974-05-07 1975-11-11 Ebara Mfg Method of joining by diffusion welding a hollow part of nonferrous metal onto the inner surface of a hollow part of ferrous metal
US4209896A (en) * 1976-04-02 1980-07-01 Texas Instruments Incorporated Method of assembly of an anti-corrosion anode connector system
US4152816A (en) * 1977-06-06 1979-05-08 General Motors Corporation Method of manufacturing a hybrid turbine rotor
US4186473A (en) * 1978-08-14 1980-02-05 General Motors Corporation Turbine rotor fabrication by thermal methods
US4231507A (en) * 1979-01-09 1980-11-04 The United States Of America As Represented By The United States Department Of Energy High-temperature, high-pressure bonding of nested tubular metallic components
FR2450631A1 (en) * 1979-03-05 1980-10-03 Sybron Corp AGITATOR WITH SEPARABLE BLADES, AND METHOD FOR MOUNTING THE BLADES ON THE SHAFT OF THE AGITATOR
DE3007718A1 (en) * 1979-03-05 1980-09-11 Sybron Corp STIRRER WITH A REMOVABLE BLADE UNIT AND METHOD FOR ITS ASSEMBLY
US4314396A (en) * 1979-03-05 1982-02-09 Sybron Corporation Separable blade agitator assembly and disassembly method
WO1989006583A1 (en) * 1988-01-14 1989-07-27 Electric Power Research Institute, Inc. High pressure bonding process
US4899923A (en) * 1988-01-14 1990-02-13 Electric Power Research Institute, Inc. High pressure bonding process
US5988484A (en) * 1998-03-20 1999-11-23 Osborn; Donald Clad tubular product and method of manufacturing same
US20100126999A1 (en) * 2008-11-21 2010-05-27 Gm Global Technology Operations, Inc. High pressure tank and method thereof
US8091203B2 (en) * 2008-11-21 2012-01-10 GM Global Technology Operations LLC High pressure tank and method thereof
US20120180299A1 (en) * 2009-07-10 2012-07-19 Progressive Ip Ltd. Integrity of the union between components

Also Published As

Publication number Publication date
GB1156977A (en) 1969-07-02
BE685169A (en) 1967-02-06
NL6611099A (en) 1967-02-07
DE1564684B2 (en) 1976-01-15
DE1564684A1 (en) 1970-07-23

Similar Documents

Publication Publication Date Title
US3559274A (en) Process for the sheathing of tubular nuclear fuel elements
US5383228A (en) Method for making fuel cladding having zirconium barrier layers and inner liners
US5517540A (en) Two-step process for bonding the elements of a three-layer cladding tube
JPH0790522A (en) Production of zircaloy pipe excellent in resistance to crack growth
JPH0717993B2 (en) A method for complete alpha recrystallization annealing of zirconium based alloy tubing by induction heating.
JPH0213280B2 (en)
JP2815551B2 (en) Method of manufacturing cladding
EP0047082A1 (en) Method of production of cladding tube for nuclear fuel element
US4613479A (en) Water reactor fuel cladding
JPS6234095A (en) Nuclear fuel coated tube
US4659540A (en) Composite construction for nuclear fuel containers
JPS62272188A (en) Composite coated tube for nuclear fuel and manufacture thereof
Sagat et al. Deformation and failure of zircaloy fuel sheaths under LOCA conditions
US3135697A (en) Method of hydriding
US4636267A (en) Vacuum annealing of zirconium based articles
US3154845A (en) Method of fabricating a fuel element
Shek et al. Metallographic and fractographic observations of hydrides during delayed hydride cracking in Zr-2.5% Nb alloy
JPS62220212A (en) Manufacture of zirconium liner tube stock
JP2500165B2 (en) Method for manufacturing fuel cladding tube
JPS6036984A (en) Nuclear reactor fuel coated pipe and manufacture thereof
Jaffe Salt Bath Heat Treatment of PWR Core 2 Fuel Elements
Liptai et al. On the formation of substructure in alpha plutonium at high pressures
Coleman et al. Cracking zirconium alloys in hydrogen
Snyder Fuel-clad Bond Testing of Zircaloy-2 Clad, Uranium-12 w/o Molybdenum Fuel Rods
Maldonado et al. PWC‐11 Fabrication Methods for Optimum Strength for SP‐100 Applications